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Gnome Lambda

From Wikipedia, the free encyclopedia
Lambda
Gnome 7 Lambda as shown in a 1913 Gnome catalog
TypeRotaryaero engine
ManufacturerGnome et Rhône
First runc. 1911
Major applications
Number built
  • 2,720 (French production)
  • 979 (British production)

TheGnome 7 Lambda was a French designed, seven-cylinder,air-cooledrotaryaero engine that was produced under license in Britain and Germany. Powering severalWorld War I-era aircraft types it was claimed to produce 80horsepower (60 kW) from itscapacity of 12 litres (730 cubic inches) although recorded figures are lower.[1]

Just under 1,000 units were produced in Britain, the majority (967) by theDaimler Company ofCoventry. A 14-cylinder variant was known as the Gnome 14 Lambda-Lambda.

In GermanyMotorenfabrik Oberursel license-built the seven-cylinder engine as theOberursel U.0 and later copied the 14-cylinder design and designated it as theOberursel U.III.

Variants

[edit]
Gnome 7 Lambda
Seven-cylinder, single-row rotary engine.
Gnome 7 Lambda (long stroke)
Increasedstroke of 145 mm (5.71 in) to raise thecompression ratio to 3.87:1, and total displacement to 12.26 litres (748 cu in).
Gnome 14 Double Lambda
14-cylinder, two-row rotary engine using Lambda cylinders. 160 hp (120 kW).
Motorenfabrik Oberursel U.0
German production of the Gnome 7 Lambda – had a 124 mm (4.88 in) cylinder bore and 140 mm (5.51 in) piston stroke for a total displacement of 11.52 litres (703 cu in), external diameter of 1.020 metres (40.16 in).[2]
Motorenfabrik Oberursel U.III
German production of the Gnome 14 Double Lambda

Applications

[edit]

List from Lumsden

TheSopwith Tabloid replica on display at theRoyal Air Force Museum is fitted with an original Gnome 7 Lambda[clarification needed] engine.

Gnome 7 Lambda

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Gnome 14 Lambda-Lambda

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Survivors

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An original Gnome 7 Lambda engine is installed in theSopwith Tabloid replica aircraft on display in theGrahame-White hall of theRoyal Air Force Museum London.[4]

Specifications (Gnome 7 Lambda)

[edit]
Oberursel U.III, a copy of the 14-cylinder Gnome Lambda-Lambda

Data fromLumsden.[1]

General characteristics

Components

  • Valvetrain: Automatic centre-piston inlet valve, overhead exhaust valve (one each per cylinder)
  • Cooling system: Air-cooled
  • Reduction gear: Direct drive, right-hand tractor, left-hand pusher

Performance

See also

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Comparable engines

Related lists

References

[edit]
Wikimedia Commons has media related toGnome Lambda andGnome Lambda-Lambda.

Notes

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  1. ^abLumsden 2003, p. 151.
  2. ^"Obsah fóra :: Zbraně a vybavení :: Výzbroj, zbraňové systémy, vybavení a příslušenství :: Motory :: Letecké motory :: Pístové :: Německo (DEU) :: Oberursel U.0".valka.cz (in Czech). 24 January 2012. RetrievedJuly 19, 2013.
  3. ^"The Borel Hydro-Monoplane".Flight: 450. 19 July 1913.
  4. ^RAF Museum – Sopwith Tabloid replica history Retrieved: 11 November 2010.

Bibliography

[edit]
  • Lumsden, Alec.British Piston Engines and their Aircraft. Marlborough, Wiltshire: Airlife Publishing, 2003.ISBN 1-85310-294-6.
Gnome rotary engines
Le Rhône rotary engines
Gnome et Rhône radial engines
Rotary engines (Gnome designs)
Rotary engines (Le Rhône designs)
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